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Heat Transfer Research
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ISSN Druckformat: 1064-2285
ISSN Online: 2162-6561

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Heat Transfer Research

DOI: 10.1615/HeatTransRes.v38.i2.50
pages 143-162

Ratio of the Thermal and Erosion Components in Heat-Erosion Destruction of Materials in a Supersonic Heterogeneous Flow

D. S. Mikhatulin
Institute of High Temperatures of the Russian Academy of Science, Moscow, Russia, 127412
Yury V. Polezhaev
Department of Heat Transfer, Institute for High Temperatures, Russian Academy of Sciences, Izhorskaya 13/19, Moscow 127412, Russia

ABSTRAKT

We consider the possibilities for modeling heat-erosion impact of a dusty atmosphere on the elements of the frontal surfaces of rockets on ground-based gasdynamic test benches, which should be reproduced in experimental investigations. A model of heat-erosion destruction of coating materials, in which the total entrainment of mass is divided into thermal, erosion, and gas-mechanical, is proposed. The conditions, when these components are independent of each other and when this dependence can be ignored, are analyzed. The determining parameters are formulated.


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